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The Cessna 140 was originally equipped with a Continental C-85-12 or C-85-12F horizontally opposed, air-cooled, four-cylinder piston engine of 85 hp (63 kW). The Continental C-90-12F or C-90-14F of 90 hp (67 kW) was optional, as was the 108 hp (81 kW) Lycoming O-235-C1 engine, an aftermarket installation authorized in the type certificate .
Cessna Model A: 1927 70 Single piston engine monoplane utility airplane Cessna Model BW: 13 Single piston engine monoplane utility airplane Cessna CG-2: Glider Cessna CH-1: 1953 ~50 Single piston engine utility helicopter Cessna CH-4: Single piston engine utility helicopter Cessna CR-1: 1 Single piston engine monoplane racer Cessna CR-2: 1930 1
Data from Jane's All The World's Aircraft 1982–83 General characteristics Crew: 1 or 2 pilots Capacity: 8–10 passengers Length: 39 ft 0 in (11.89 m) Wingspan: 49 ft 4 in (15.04 m) Height: 13 ft 2 in (4.01 m) Wing area: 253.6 sq ft (23.56 m 2) Aspect ratio: 9.6:1 Airfoil: NACA 23018 at root, NACA 23019 at tip Empty weight: 5,682 lb (2,577 kg) Gross weight: 9,850 lb (4,468 kg) Powerplant: 2 ...
The Cessna Citation Longitude is a business jet produced by Cessna, part of the Cessna Citation family. It remains the largest business jet by Cessna. It remains the largest business jet by Cessna. Announced at the May 2012 EBACE , the Model 700 made its first flight on October 8, 2016, with certification obtained in September 2019.
Data from Jane's All The World's Aircraft 1969–70 General characteristics Crew: 1 Capacity: 5 passengers Length: 29 ft 9 in (9.07 m) Wingspan: 38 ft 09 in (11.81 m) Height: 9 ft 4 in (2.84 m) Wing area: 201 sq ft (18.7 m 2) Aspect ratio: 7.18:1 Airfoil: NACA 2412 at root, NACA 2409 at tip Empty weight: 2,655 lb (1,204 kg) Max takeoff weight: 4,400 lb (1,996 kg) Fuel capacity: 92 US gal (77 ...
This is the speed at which drag is minimised. For jet aircraft, "long-range cruise" speed (LRC) is defined as the speed which gives 99% of the maximum range, for a given weight. This results in a 3–5% increase in speed. [8] It is also a more stable speed than maximum range speed, so gives less autothrottle movement. [9]
Data from Jane's All the World's Aircraft 1993–94 General characteristics Crew: Two pilots (One pilot on II/SP) Capacity: Six to eight passengers Length: 47 ft 8 + 1 ⁄ 2 in (14.542 m) Wingspan: 52 ft 2 + 1 ⁄ 2 in (15.913 m) Height: 15 ft 0 in (4.57 m) Wing area: 342.6 sq ft (31.83 m 2) Airfoil: NACA 23000 Empty weight: 8,059 lb (3,656 kg) Max takeoff weight: 15,100 lb (6,849 kg) Fuel ...
The C90 was introduced in 1947 as a follow-on to the A65, which had been in production since 1939. [7] [8] Many of the designs powered by the C90 are upgraded variants of earlier A65 powered designs, such as the Piper J-3 Cub and PA-11 Cub Special, [9] Aeronca 7AC, [3] and Luscombe 8A. [10] The engine was developed from the earlier O-190 by increasing the stroke 1 ⁄ 4 inch.
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